FR2424414A1 - Circuit de regulation de vitesse non lineaire pour un groupe turbine a gaz/alternateur - Google Patents
Circuit de regulation de vitesse non lineaire pour un groupe turbine a gaz/alternateurInfo
- Publication number
- FR2424414A1 FR2424414A1 FR7910328A FR7910328A FR2424414A1 FR 2424414 A1 FR2424414 A1 FR 2424414A1 FR 7910328 A FR7910328 A FR 7910328A FR 7910328 A FR7910328 A FR 7910328A FR 2424414 A1 FR2424414 A1 FR 2424414A1
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- speed
- speed regulation
- linear speed
- regulation circuit
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/02—Purpose of the control system to control rotational speed (n)
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/06—Purpose of the control system to match engine to driven device
- F05D2270/061—Purpose of the control system to match engine to driven device in particular the electrical frequency of driven generator
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Eletrric Generators (AREA)
- Control Of Turbines (AREA)
Abstract
L'INVENTION CONCERNE LES CIRCUITS DE COMMANDE DES GROUPES TURBINE A GAZALTERNATEUR. UN CIRCUIT DE REGULATION DE VITESSE POUR TURBINE A GAZ FOURNIT UN SIGNAL DE SORTIE QUI PRESENTE UNE RELATION NON LINEAIRE ENTRE LA TENSION DE SORTIE V ET LA VITESSE DE ROTATION DE LA TURBINE, EXPRIMEE EN POURCENTAGE DE LA VITESSE SYNCHRONE. CETTE CARACTERISTIQUE PERMET DE RAMENER PLUS RAPIDEMENT LA VITESSE DANS LES LIMITES DE REGULATION DESIREES EN CAS DE VARIATION IMPORTANTE DE LA CHARGE DE L'ALTERNATEUR. APPLICATION A LA PRODUCTION D'ENERGIE ELECTRIQUE.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/899,795 US4188781A (en) | 1978-04-25 | 1978-04-25 | Non-linear dual mode regulator circuit |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2424414A1 true FR2424414A1 (fr) | 1979-11-23 |
FR2424414B1 FR2424414B1 (fr) | 1984-03-16 |
Family
ID=25411576
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7910328A Granted FR2424414A1 (fr) | 1978-04-25 | 1979-04-24 | Circuit de regulation de vitesse non lineaire pour un groupe turbine a gaz/alternateur |
Country Status (7)
Country | Link |
---|---|
US (1) | US4188781A (fr) |
JP (1) | JPS54158507A (fr) |
DE (1) | DE2916629A1 (fr) |
FR (1) | FR2424414A1 (fr) |
GB (1) | GB2019618B (fr) |
IT (1) | IT1112868B (fr) |
NL (1) | NL7903120A (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2465879A1 (fr) * | 1979-09-21 | 1981-03-27 | Lucas Industries Ltd | Installation a regulateur hydromecanique de debit de carburant pour moteur a turbine a gaz comportant un circuit d'avance de phase |
FR2529682A1 (fr) * | 1982-07-02 | 1984-01-06 | Gen Electric | Systeme de controle de source de courant |
Families Citing this family (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2032142B (en) * | 1978-10-02 | 1982-11-03 | Lucas Industries Ltd | Fuel control for a multi-engine gas turbine installation |
JPS55109729A (en) * | 1979-02-16 | 1980-08-23 | Nissan Motor Co Ltd | Fuel control device for gas turbine |
GB2081934B (en) * | 1980-08-08 | 1984-03-07 | Ass Eng Ltd | Automatic speed control systems |
US4593523A (en) * | 1980-12-17 | 1986-06-10 | Allied Corporation | Method and apparatus for acceleration limiting a gas turbine engine |
US4432201A (en) * | 1981-01-14 | 1984-02-21 | Aviation Electric Ltd. | Acceleration limit reset |
US4442667A (en) * | 1981-01-14 | 1984-04-17 | Aviation Electric Ltd. | Acceleration limit reset |
US4697238A (en) * | 1981-01-21 | 1987-09-29 | Teledyne Industries, Inc. | Integrated fuel management system |
US4441156A (en) * | 1981-01-21 | 1984-04-03 | Teledyne Industries, Inc. | Integrated fuel management system |
US4449360A (en) * | 1981-04-30 | 1984-05-22 | Aviation Electric Ltd. | Stall detector and surge prevention feature for a gas turbine engine |
US4507915A (en) * | 1981-04-30 | 1985-04-02 | Allied Corporation | Stall detector and surge prevention feature for a gas turbine engine |
US4417440A (en) * | 1981-05-12 | 1983-11-29 | Aviation Electric Ltd. | Fuel control apparatus for a gas turbine engine |
US4422289A (en) * | 1981-05-12 | 1983-12-27 | Aviation Electric Ltd. | Fuel control apparatus for a gas turbine engine |
US4517797A (en) * | 1981-05-25 | 1985-05-21 | Hitachi, Ltd. | Fuel control method for gas turbine |
FR2517751A1 (fr) * | 1981-12-04 | 1983-06-10 | Neyrpic | Procede et dispositif pour minimiser l'ecart dynamique de la vitesse dans un systeme de regulation de vitesse d'une turbine hydraulique |
JPS6275030A (ja) * | 1985-09-26 | 1987-04-06 | Hitachi Ltd | 発電機用原動機の速度・負荷制御装置 |
JPS62247799A (ja) * | 1986-04-18 | 1987-10-28 | Toyota Motor Corp | ガスタ−ビン発電機の制御装置 |
US4783957A (en) * | 1986-12-23 | 1988-11-15 | Sundstrand Corporation | Fuel control circuit for a turbine engine |
US4845943A (en) * | 1988-04-29 | 1989-07-11 | United Technologies Corporation | Control method for topping loop |
US4884397A (en) * | 1988-04-29 | 1989-12-05 | United Technologies Corporation | Control system topping loop |
JPH02111144A (ja) * | 1988-10-19 | 1990-04-24 | Mitsubishi Electric Corp | 電話番号登録装置 |
US4928484A (en) * | 1988-12-20 | 1990-05-29 | Allied-Signal Inc. | Nonlinear multivariable control system |
US4993221A (en) * | 1988-12-21 | 1991-02-19 | General Electric Company | Gas turbine engine control system |
JPH02267328A (ja) * | 1989-03-20 | 1990-11-01 | General Electric Co <Ge> | ガスタービンエンジンの制御装置および制御方法 |
JPH02245901A (ja) * | 1989-03-20 | 1990-10-01 | Noboru Yamaguchi | 制御方法および制御装置 |
US5197280A (en) * | 1989-03-20 | 1993-03-30 | General Electric Company | Control system and method for controlling a gas turbine engine |
US5029441A (en) * | 1989-09-20 | 1991-07-09 | United Technologies Corporation | Dynamic compensation to n-dot schedules |
JP3684208B2 (ja) * | 2002-05-20 | 2005-08-17 | 株式会社東芝 | ガスタービン制御装置 |
WO2004053312A1 (fr) * | 2002-12-12 | 2004-06-24 | Ebara Corporation | Appareil a turbine a gaz |
EP2014880A1 (fr) * | 2007-07-09 | 2009-01-14 | Universiteit Gent | Système combiné de génération de chaleur amélioré |
US8499874B2 (en) | 2009-05-12 | 2013-08-06 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
WO2011109514A1 (fr) | 2010-03-02 | 2011-09-09 | Icr Turbine Engine Corporatin | Puissance à répartir à partir d'une installation d'énergie renouvelable |
US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
WO2012031297A2 (fr) | 2010-09-03 | 2012-03-08 | Icr Turbine Engine Corporation | Configurations de moteur à turbine à gaz |
US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
US9562479B2 (en) | 2013-03-13 | 2017-02-07 | General Electric Company | Systems and methods of droop response control of turbines |
US9932850B2 (en) * | 2015-02-03 | 2018-04-03 | General Electric Company | Correction system and method for gas turbine proportional droop governor |
TWI574141B (zh) * | 2015-12-08 | 2017-03-11 | 新唐科技股份有限公司 | 雙模穩壓器電路 |
KR101893689B1 (ko) * | 2017-04-26 | 2018-08-30 | 두산중공업 주식회사 | 가스터빈 시스템 및 제어 방법 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB791054A (en) * | 1953-12-14 | 1958-02-19 | Gen Electric | Improvements in electric control systems |
GB1107523A (en) * | 1964-06-10 | 1968-03-27 | United Aircraft Corp | Control circuit for servo mechanisms |
US3520133A (en) * | 1968-03-14 | 1970-07-14 | Gen Electric | Gas turbine control system |
US4077204A (en) * | 1973-10-23 | 1978-03-07 | Nissan Motor Company, Limited | Control system for a gas turbine engine |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB962801A (en) * | 1959-07-17 | 1964-07-01 | Dehavilland Aircraft | Improvements in or relating to engine control systems |
JPS5032886B2 (fr) * | 1972-03-31 | 1975-10-25 | ||
US3854287A (en) * | 1973-12-26 | 1974-12-17 | United Aircraft Corp | Self-trimming control for turbofan engines |
US4010605A (en) * | 1974-08-08 | 1977-03-08 | Westinghouse Electric Corporation | Accurate, stable and highly responsive gas turbine startup speed control with fixed time acceleration especially useful in combined cycle electric power plants |
-
1978
- 1978-04-25 US US05/899,795 patent/US4188781A/en not_active Expired - Lifetime
-
1979
- 1979-04-06 GB GB7912115A patent/GB2019618B/en not_active Expired
- 1979-04-19 IT IT22005/79A patent/IT1112868B/it active
- 1979-04-20 NL NL7903120A patent/NL7903120A/xx not_active Application Discontinuation
- 1979-04-23 JP JP4918179A patent/JPS54158507A/ja active Granted
- 1979-04-24 FR FR7910328A patent/FR2424414A1/fr active Granted
- 1979-04-25 DE DE19792916629 patent/DE2916629A1/de not_active Withdrawn
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB791054A (en) * | 1953-12-14 | 1958-02-19 | Gen Electric | Improvements in electric control systems |
GB1107523A (en) * | 1964-06-10 | 1968-03-27 | United Aircraft Corp | Control circuit for servo mechanisms |
US3520133A (en) * | 1968-03-14 | 1970-07-14 | Gen Electric | Gas turbine control system |
US4077204A (en) * | 1973-10-23 | 1978-03-07 | Nissan Motor Company, Limited | Control system for a gas turbine engine |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2465879A1 (fr) * | 1979-09-21 | 1981-03-27 | Lucas Industries Ltd | Installation a regulateur hydromecanique de debit de carburant pour moteur a turbine a gaz comportant un circuit d'avance de phase |
FR2529682A1 (fr) * | 1982-07-02 | 1984-01-06 | Gen Electric | Systeme de controle de source de courant |
Also Published As
Publication number | Publication date |
---|---|
GB2019618A (en) | 1979-10-31 |
FR2424414B1 (fr) | 1984-03-16 |
US4188781A (en) | 1980-02-19 |
JPS54158507A (en) | 1979-12-14 |
GB2019618B (en) | 1982-10-27 |
DE2916629A1 (de) | 1979-10-31 |
IT1112868B (it) | 1986-01-20 |
NL7903120A (nl) | 1979-10-29 |
IT7922005A0 (it) | 1979-04-19 |
JPS6331653B2 (fr) | 1988-06-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |